Gemini II
Audio With External Links Item Preview
Share or Embed This Item
The Gemini II mission. The audio files are named as per their original historical audio reel number at the NASA historical audio vault. Information listed below is the sum-total of data on these files.
MISSION INFORMATION:
Gemini II
Pad LC-19 (17)
Titan-II (2)
Crew: Unmanned
Payload: Gemini-II capsule
Altitude: 171.1 km (92.4nm)
Inclination: TBD
Orbits: suborbital
Duration: 0 Days, 0 hours, 18 min, 16 seconds
Distance: 3422.4km (1848 nm)
Mission Objective
Demonstrate reentry heat protection during maximum heating reentry; Demonstrate structural integrity of spacecraft; Demonstrate satisfactory performance of major subsystems; Demonstrate checkout and launch procedures; Evaluate backup guidance steering signals through launch.
Secondary objectives included: Obtain test results on fuel cell and reactant supply, cryogenics, and communications systems; Demonstrate and further flight-qualify GLV and spacecraft from countdown thru insertion. Train flight controllers and qualify ground communications tracking system.
Launch: January 19, 1965 9:03:59.861 am EST
Landing: January 19, 1965 9:22:14
Landed at 16deg 36m North Latitude and 49deg 46m West in Atlantic ocean. Miss distance from planned landing point 62.9km.
The Titan II/Gemini launch vehicle had to be dismantled to protect it from 2 hurricanes in August and September of 1964. The 2nd stage of the vehicle was taken down and stored in a hanger on 26 August 1964 in preparation for Hurricane Cleo, but the entire launch vehicle was dismantled and removed from Pad 19 in early September before Hurricane Dora passed over the Cape on September 9th. The Gemini launch vehicle was erected for the final time on Pad 19 on 12 September 1964
Gemini-II had been scheduled for launch December 9, 1964. On that date the countdown reached zero and the stage one engines were ignited. The launch vehicle's Malfunction Detection System detected technical problems due to a loss of hydraulic pressure and shutdown the engines about one second after ignition.
Mission Highlights
All primary mission objectives were achieved. All secondary objectives except fuel cell test were achieved. Fuel cell deactivated before liftoff.
Digitized, cataloged and archived by the Houston Audio Control Room, at the NASA Johnson Space Center.
MISSION INFORMATION:
Gemini II
Pad LC-19 (17)
Titan-II (2)
Crew: Unmanned
Payload: Gemini-II capsule
Altitude: 171.1 km (92.4nm)
Inclination: TBD
Orbits: suborbital
Duration: 0 Days, 0 hours, 18 min, 16 seconds
Distance: 3422.4km (1848 nm)
Mission Objective
Demonstrate reentry heat protection during maximum heating reentry; Demonstrate structural integrity of spacecraft; Demonstrate satisfactory performance of major subsystems; Demonstrate checkout and launch procedures; Evaluate backup guidance steering signals through launch.
Secondary objectives included: Obtain test results on fuel cell and reactant supply, cryogenics, and communications systems; Demonstrate and further flight-qualify GLV and spacecraft from countdown thru insertion. Train flight controllers and qualify ground communications tracking system.
Launch: January 19, 1965 9:03:59.861 am EST
Landing: January 19, 1965 9:22:14
Landed at 16deg 36m North Latitude and 49deg 46m West in Atlantic ocean. Miss distance from planned landing point 62.9km.
The Titan II/Gemini launch vehicle had to be dismantled to protect it from 2 hurricanes in August and September of 1964. The 2nd stage of the vehicle was taken down and stored in a hanger on 26 August 1964 in preparation for Hurricane Cleo, but the entire launch vehicle was dismantled and removed from Pad 19 in early September before Hurricane Dora passed over the Cape on September 9th. The Gemini launch vehicle was erected for the final time on Pad 19 on 12 September 1964
Gemini-II had been scheduled for launch December 9, 1964. On that date the countdown reached zero and the stage one engines were ignited. The launch vehicle's Malfunction Detection System detected technical problems due to a loss of hydraulic pressure and shutdown the engines about one second after ignition.
Mission Highlights
All primary mission objectives were achieved. All secondary objectives except fuel cell test were achieved. Fuel cell deactivated before liftoff.
Digitized, cataloged and archived by the Houston Audio Control Room, at the NASA Johnson Space Center.
- Addeddate
- 2010-12-01 23:54:26
- Color
- color
- External-identifier
-
urn:storj:bucket:jvrrslrv7u4ubxymktudgzt3hnpq:GeminiIi
- Identifier
- GeminiIi
- Ocr
- ABBYY FineReader 9.0
- Ocr_converted
- abbyy-to-hocr 1.1.20
- Ocr_module_version
- 0.0.16
- Ppi
- 300
- Sound
- sound
comment
Reviews
There are no reviews yet. Be the first one to
write a review.
2,749 Views
1 Favorite
DOWNLOAD OPTIONS
IN COLLECTIONS
NASAUploaded by John Stoll on